MIL-S-6252 Specifications, Detail, Fixed Wing Aircraft, Preparation Of S/S By Mil-Std-832This specification contains instruction to be followed in the preparation of detail specifications for the complete aircraft.

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MII-8-6252.0

Aft LE of MAC               percent  MAC

3.1.5  Areas.    (Items   may  be  added,  omitted,  or  modified  in  this paragraph  to properly  describe the aircraft.  The following informaD tion  is not to be used for  inspection purposes.)

Wing  area,  total,  including  ailerons,  flaps  and

-square        feet  of fuelage  or hull                    -square         feet

Wing flap area,  aft  of hinge  line, total...             --square       feet

Aileron  area,   aft  of  hinge  line,  but  including overhanging        external    balance   t6rward    of hinge,  total  including        square  feet  of  tab

area                                                                        =uare           feet

Horizontal  tail  area,  total...                                   --square       feet stabilizer,   (to  elevator  hinge),  excluding  over-

hanging   elevator  balance  and  including-- square feet  of fuselage  or hull  and        square

feet  of contained  elevator  balance                     --square       feet

Elevator,  aft  of hinge,  but  including-square feet  of overhanging  external  balance forward

of hinge and         square  feet  of tab area          -square        feet

Vertical  tail  area;  total...                    =                  --sqiiare       feet

Fin,  (to   rudder 'hinge) ,  excluding overhanging rudder  balance  and  including         square  feet

of contained rudder  balance                              -square        feet

Rudder,  aft  of  hinge,  but  including        square feet  of overhanging  external  balance forward

of  hinge  and         square  feet  of tab  area        ---square     feet

3.1.6 Dimensions  and  general  data.  (Items may be added, omitj.ed, or modified in this  paragraph  to  properly  describe the  aircraft.  The following information  is not to  be  used for inspection  purposes.)

Wings:

Span,  maximum                                                        ----feet

Span, wings  folded                    ."                              .                feet

Chord:

At root                                                                    ----inches

At  construction  tip  (theoretical  extended  sec-

tion  at  tip)                                                         ----inches

Mean aerodynamic  . .. . . . .   . . .   .             . . . .... . . . . .. .. .                inches

Airfoil  section  designation  and  thickness   (per-

cent  chord)                                                             ----

t

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